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<title> NACA 63-430 (Velux Measurements) </title></head>

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<H1>NACA 63-430 AIRFOIL</H1>
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Reynolds number = 1.5 x 10^6 <br><br>

Measured at Velux wind tunnel (see <A
HREF="./../HTML/biblio.htm#FuglsangADM">Fuglsang, Antoniou, Dahl
and Madsen</A>) <br><br>

More details on computations and experimental facilities can be found in
the <A HREF="./../HTML/report.htm"><font color="#006699">Wind Turbine
Airfoil Catalogue</font></A>.


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<H1>DATA AVAILABLE:</H1><p><p>

- <A HREF="./prof.dat"> Airfoil shape </A><p>

<font size=+3> Experiments:<br> </font>
- <A HREF="./cldm.exp"> Lift, Drag and Moment Coefficients </A><p>

- <A HREF="./cp_06.518.exp"> Pressure Distribution - Angle of Attack = 06.518 deg. </A><br>
- <A HREF="./cp_08.628.exp"> Pressure Distribution - Angle of Attack = 08.628 deg. </A><br>
- <A HREF="./cp_10.602.exp"> Pressure Distribution - Angle of Attack = 10.602 deg. </A><br>
- <A HREF="./cp_13.535.exp"> Pressure Distribution - Angle of Attack = 13.535 deg. </A><br>
- <A HREF="./cp_16.290.exp"> Pressure Distribution - Angle of Attack = 16.290 deg. </A><br>
- <A HREF="./cp_20.617.exp"> Pressure Distribution - Angle of Attack = 20.617 deg. </A><p>

<font size=+3> XFOIL Computations:<br> </font>
- <A HREF="./cldm.xf"> Lift, Drag and Moment Coefficients </A><p>
- <A HREF="./cfp_06.518.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 06.518 deg. </A><br>
- <A HREF="./cfp_08.628.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 08.628 deg. </A><br>
- <A HREF="./cfp_10.602.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 10.602 deg. </A><br>
- <A HREF="./cfp_13.535.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 13.535 deg. </A><br>
- <A HREF="./cfp_16.290.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 16.290 deg. </A><br>
- <A HREF="./cfp_20.617.xf"> Skin Friction and Pressure Distributions - Angle of Attack = 20.617 deg. </A><p>

<font size=+3> EllipSys2D Computations: </font><p>
<font size=+2><em>* Fully turbulent:</em><br> </font>
- <A HREF="./FULLYTURB/cldm.ellipsys"> Lift, Drag and Moment Coefficients </A><p>
- <A HREF="./FULLYTURB/cp_06.518.ellipsys"> Pressure Distribution - Angle of Attack = 06.518 deg. </A><br>
- <A HREF="./FULLYTURB/cp_08.628.ellipsys"> Pressure Distribution - Angle of Attack = 08.628 deg. </A><br>
- <A HREF="./FULLYTURB/cp_10.602.ellipsys"> Pressure Distribution - Angle of Attack = 10.602 deg. </A><br>
- <A HREF="./FULLYTURB/cp_13.535.ellipsys"> Pressure Distribution - Angle of Attack = 13.535 deg. </A><br>
- <A HREF="./FULLYTURB/cp_16.290.ellipsys"> Pressure Distribution - Angle of Attack = 16.290 deg. </A><br>
- <A HREF="./FULLYTURB/cp_20.617.ellipsys"> Pressure Distribution - Angle of Attack = 20.617 deg. </A><p>

- <A HREF="./FULLYTURB/cf_06.518.ellipsys"> Skin Friction Distribution - Angle of Attack = 06.518 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_08.628.ellipsys"> Skin Friction Distribution - Angle of Attack = 08.628 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_10.602.ellipsys"> Skin Friction Distribution - Angle of Attack = 10.602 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_13.535.ellipsys"> Skin Friction Distribution - Angle of Attack = 13.535 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_16.290.ellipsys"> Skin Friction Distribution - Angle of Attack = 16.290 deg. </A> <br>
- <A HREF="./FULLYTURB/cf_20.617.ellipsys"> Skin Friction Distribution - Angle of Attack = 20.617 deg. </A> <p>

<font size=+2><em>* With transition model:</em><br> </font>
- <A HREF="./TRANSITION/cldm.ellipsys"> Lift, Drag and Moment Coefficients </A><p>
- <A HREF="./TRANSITION/cp_06.518.ellipsys"> Pressure Distribution - Angle of Attack = 06.518 deg. </A><br>
- <A HREF="./TRANSITION/cp_08.628.ellipsys"> Pressure Distribution - Angle of Attack = 08.628 deg. </A><br>
- <A HREF="./TRANSITION/cp_10.602.ellipsys"> Pressure Distribution - Angle of Attack = 10.602 deg. </A><br>
- <A HREF="./TRANSITION/cp_13.535.ellipsys"> Pressure Distribution - Angle of Attack = 13.535 deg. </A><br>
- <A HREF="./TRANSITION/cp_16.290.ellipsys"> Pressure Distribution - Angle of Attack = 16.290 deg. </A><br>
- <A HREF="./TRANSITION/cp_20.617.ellipsys"> Pressure Distribution - Angle of Attack = 20.617 deg. </A><p>

- <A HREF="./TRANSITION/cf_06.518.ellipsys"> Skin Friction Distribution - Angle of Attack = 06.518 deg. </A> <br>
- <A HREF="./TRANSITION/cf_08.628.ellipsys"> Skin Friction Distribution - Angle of Attack = 08.628 deg. </A> <br>
- <A HREF="./TRANSITION/cf_10.602.ellipsys"> Skin Friction Distribution - Angle of Attack = 10.602 deg. </A> <br>
- <A HREF="./TRANSITION/cf_13.535.ellipsys"> Skin Friction Distribution - Angle of Attack = 13.535 deg. </A> <br>
- <A HREF="./TRANSITION/cf_16.290.ellipsys"> Skin Friction Distribution - Angle of Attack = 16.290 deg. </A> <br>
- <A HREF="./TRANSITION/cf_20.617.ellipsys"> Skin Friction Distribution - Angle of Attack = 20.617 deg. </A>


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<H1>FIGURES AVAILABLE: (PostScript files)</H1><p><p>

- <A HREF="./PS/profile.ps"> Airfoil shape </A><p>

- <A HREF="./PS/cl.ps"> Lift Coefficient </A><br>
- <A HREF="./PS/cd.ps"> Drag Coefficient </A><br>
- <A HREF="./PS/cm.ps"> Moment Coefficient </A><p>

- <A HREF="./PS/cp_a06.518.ps"> Pressure Distribution - Angle of Attack = 06.518 deg. </A><br>
- <A HREF="./PS/cp_a08.628.ps"> Pressure Distribution - Angle of Attack = 08.628 deg. </A><br>
- <A HREF="./PS/cp_a10.602.ps"> Pressure Distribution - Angle of Attack = 10.602 deg. </A><br>
- <A HREF="./PS/cp_a13.535.ps"> Pressure Distribution - Angle of Attack = 13.535 deg. </A><br>
- <A HREF="./PS/cp_a16.290.ps"> Pressure Distribution - Angle of Attack = 16.290 deg. </A><br>
- <A HREF="./PS/cp_a20.617.ps"> Pressure Distribution - Angle of Attack = 20.617 deg. </A><p>

- <A HREF="./PS/cf_a06.518.ps"> Skin Friction Distribution - Angle of Attack = 06.518 deg. </A><br>
- <A HREF="./PS/cf_a08.628.ps"> Skin Friction Distribution - Angle of Attack = 08.628 deg. </A><br>
- <A HREF="./PS/cf_a10.602.ps"> Skin Friction Distribution - Angle of Attack = 10.602 deg. </A><br>
- <A HREF="./PS/cf_a13.535.ps"> Skin Friction Distribution - Angle of Attack = 13.535 deg. </A><br>
- <A HREF="./PS/cf_a16.290.ps"> Skin Friction Distribution - Angle of Attack = 16.290 deg. </A><br>
- <A HREF="./PS/cf_a20.617.ps"> Skin Friction Distribution - Angle of Attack = 20.617 deg. </A><p>



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